In situ turret bearing remediation and assembly

ABSTRACT

In a three row, roller bearing assembly coupling a vessel to a turret, the bearing assembly having a support row assembly disposed between an inner ring connected to the turret and outer rings connected to the vessel, a method and arrangement for in situ remediation of a damaged support row assembly. Couplers are secured to existing inner ring stud bolts. A continuous bearing ring below the couplers is assembled and a support bearing arrangement is installed between the couplers and the bearing ring. Reaction plates are mounted to the vessel. Each reaction plate has a jack screw which is positioned directly below the bearing ring. The jack screws are turned to elevate the bearing ring and form a flat surface for support of the support bearing arrangement. The turret axial load is transferred from the damaged support row assembly to the support bearing arrangement.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation of co-pending U.S. patent applicationSer. No. 15/813,981, filed on Nov. 15, 2017, which is incorporated byreference herein.

BACKGROUND OF THE INVENTION 1. Field of the Invention

This invention relates to a turret structure for vessels such asoffshore drilling or production vessels, and more particularly to aturret bearing assembly and bearing repair procedure that can beperformed in situ.

2. Description of the Related Art

Vessel mooring systems are known in the art in which a vessel mayweathervane about a turret that is moored to the sea floor. The turretextends through a moon pool or cylindrical opening that extends throughthe hull of the vessel. The vessel is supported for rotation withrespect to the turret by turret bearing structures placed between theturret and the vessel. Horizontal and vertical bearings transferhorizontal and vertical loads between the turret and the vessel.

U.S. Pat. No. 8,671,864, issued on Mar. 18, 2014, in the names ofLindblade et al., discloses such a turret mooring system. FIG. 1 of the'864 patent discloses a bow of a vessel having a moon pool extendingthrough the vessel hull. Mounted within the moon pool is a turret aboutwhich the vessel weather vanes. The moon pool is normally of a circularcross-section, and the turret is typically of a cylindrical shape to fitwithin the moon pool. Anchor legs are connected to the turret andsecured to the sea bed by suitable anchors to restrict rotation of theturret. Risers extend from subsea wellheads or distribution facilitieson the sea floor and are connected to the turret. A manifold deck issupported on the upper end of the turret and includes valves connectedto the risers. A swivel stack extends upwardly from the turret andmanifold deck, and allows fluids to be transferred from the turret tothe vessel. The turret is supported on the vessel by a turret bearingassembly.

One type of turret bearing assembly commonly used is an integratedthree-row roller bearing assembly as shown and described in U.S. Pat.No. 5,893,784, issued on Apr. 13, 1999, to Boatman. The three-row rollerbearing assembly includes a circular array of support rollers radiallyaligned about the turret for supporting the turret weight. Any upliftingturret force is resisted by a second set of radially aligned rollers. Athird set of rollers, coaxially aligned about the turret, serves totransfer radial loads between the vessel and the turret. The threebearing rows of the three-row roller bearing assembly are preferablylubricated and sealed within a common volume by seals to provideprotection from the elements and prevent corrosion. The integratedthree-row roller bearing assembly is a precise assembly that requires ahigh degree of flatness for proper load distribution and is somewhatintolerant of distortions and deflections, which cause high pointloading stresses on select rollers.

Most three-row roller bearing assemblies on turret systems locatedoffshore are not replaceable or repairable in situ due to factors suchas the size, weight and access to the various components. Although thesebearing assemblies are designed for the life of the system, if they failor exhibit problems, no design or method exists to correct majorproblems on location. Since large vertical loads are always on thebearing support row, this is where wear problems are most likely tooccur.

U.S. Pat. No. 8,197,293, assigned to Bluewater Energy Services B.V.,discloses initially installing a secondary bearing assembly in place andloading the secondary bearing assembly when the primary bearing assemblyno longer functions. One drawback to this is that including two bearingassemblies (one as a spare) is cost prohibitive and adversely affectscapital expense.

It would be desirable to be able to replace or repair a damaged turretthree-row roller bearing assembly in situ. It would also be desirable tobe able to replace or repair a damaged turret three-row roller bearingassembly while the vessel stays on station. It would be desirable to beable to remove the large vertical load from the existing bearing supportrow and allow the vessel to stay on station. It would be desirable to beable to provide a new vertical load path in situ while allowing thevessel to weather vane about the turret.

SUMMARY OF THE INVENTION

The invention provides a repair to a turret bearing assembly withdamaged support row rollers and/or support race. The repair can beperformed and assembled in situ offshore and transfers the load off themain turret bearing's support race and onto a new replacement race in asingle lift sequence, thereby simplifying the operation and minimizingthe timeframe to perform the load transfer. Additionally, thearrangement removes the need to uninstall the vessel from its offshorelocation to perform remedial work on the damaged bearing assembly,thereby relieving the vessel's owner of considerable risk and costimplications.

An aspect of the invention is removing axial load from an in placedamaged three-row roller bearing assembly and allowing the vessel tocontinue to weather vane in either a free-state or with assistance. Theinvention removes load from the existing bearing support row andtransfers it to a remedial bearing support row. Radial load willcontinue to be transferred through the main bearing.

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

The invention is better understood by reading the detailed descriptionof embodiments which follow and by examining the accompanying drawings,in which:

FIG. 1 is a partial elevation view in cross-section of a prior artintegrated three-row roller bearing assembly for rotatively coupling aturret within a moon pool of a vessel, showing upper and lowerarrangements of radially aligned rollers for transferring axial forcesand a mid co-axial arrangement of rollers for transferring radial loadsall collocated within a single sealed, lubricated volume;

FIGS. 2 and 3 are partial perspective views in cross-section of athree-row roller bearing assembly arrangement repaired with a plainbearing according to a preferred embodiment of the present invention,the figures also showing portions of the vessel supporting structure andturret structure;

FIG. 4 is a partial elevation view in cross-section of the repairedthree-row roller bearing assembly arrangement according to theembodiment shown in FIGS. 2 and 3 without the use of a spreader bar;

FIGS. 5 and 6 are partial perspective views in cross-section of athree-row roller bearing assembly arrangement repaired with a rollerbearing according to a second preferred embodiment of the presentinvention, the figures also showing portions of the vessel supportingstructure and turret structure;

FIG. 7 is a partial elevation view in cross-section of the repairedthree-row roller bearing assembly arrangement according to theembodiment shown in FIGS. 5 and 6; and

FIG. 8 is an enlarged partial elevation view of the support rollerbearing assembly according to the second preferred embodiment.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1 depicts a cross-sectional view of a typical three race rollerbearing assembly 10 presently found in use on many turret systems. Inthis system, the turret has a single three race roller bearing assembly10 installed to react all loading acting between the turret and turretsupporting structure 14 of a floating vessel. It is to be understoodthat the turret supporting structure 14 is part of the floating vesseland has no movement relative to the floating vessel. The turret,represented by turret structure 12, is geostationary and the floatingvessel (including the turret supporting structure 14) is allowed toweather vane about the geostationary turret. The bearing assembly 10 isthe only means of load transfer across this rotational interface for anexternal turret, or an internal turret without a lower bearing.

The three-row roller bearing assembly 10 includes a circular array ofsupport rollers with support race and cage, all generally designated assupport row assembly 20. The circular array of support rollers areradially aligned about the turret for supporting the turret weight. Anyuplifting turret force is resisted by a second set of radially alignedrollers with uplift race and cage, all generally designated as upliftrow assembly 40. A third set of rollers with radial race and cage orspacers, all generally designated as radial row assembly 60, coaxiallyaligned about the turret, serve to transfer radial loads between thevessel and the turret. The third set of rollers for transferring theradial load typically have spacers between the rollers. However,sometimes the bearings are designed full complement, meaning there areno radial cages or spacers and just rollers.

The lower support roll assembly 20 is the most loaded when a downwardlyacting axial force is applied. Of the three rows of roller bearings, thebearing support rollers and races of the support roll assembly 20typically receive the most load and are the most likely to sustaindamage in medium to deep water systems. For shallow water systems, theradial load can be quite high and the vertical load nominal. Thus, inshallow water systems, the bearing radial rollers and races 60 may bethe most loaded and the most likely to sustain damage. The preferredembodiments primarily address remediation or replacement of the supportrace and rollers 20.

The bearing race provides a path on which the rollers roll. To realizethe longest service life, the roller path of the bearing race needs tobe as flat and circular as possible allowing for a smooth loaddistribution upon the rollers themselves.

Referring to FIG. 1, a bearing inner ring 30 is secured to the turretstructure 12 via a plurality of circumferentially-spaced inner ringfasteners, preferably threaded stud bolts 32, washers 36, and nuts 34. Abearing outer upper ring 42 and outer lower ring 22 are secured to theturret supporting structure 14 of the floating vessel via a plurality ofcircumferentially-spaced outer ring fasteners, preferably threaded studbolts 46 and nuts 44.

The preferred embodiments of the present invention address the in siturepair or remediation of a three-row roller bearing assembly 10 in whichthe support row assembly 20 is damaged. The preferred embodiments have agoal of in situ repair or remediation while allowing the vessel tocontinue to weather vane in either a free-state or with assistance. Thepreferred embodiments employ either rolling elements or self-lubricatingsliding bearing pads (i.e., plain bearings) to remove the axial loadfrom the main support row assembly 20. In the preferred embodiments, theaxial load is taken underneath the existing bearing assembly 10 from thebearing inner ring 30 to the outer turret supporting structure 14. Theaxial load is preferably transferred or re-routed from the damagedsupport row assembly 20 of the existing three row roller bearingassembly 10 to a new support bearing assembly (i.e., either a plainbearing assembly 100 as shown in FIGS. 2-4 or a support roller bearingassembly 200 as shown in FIGS. 5-7) with jack screws or hydraulic jacksas discussed below. Radial load will continue to be transferred throughthe existing main bearing assembly 10.

In one preferred embodiment, the plain bearing assembly 100 is installedbeneath the existing main bearing assembly 10 as shown in FIGS. 2-4.Upon installation of the plain bearing assembly 100, the plain bearingassembly 100 removes the vertical and moment load off the existingsupport row assembly 20 while the radial load path remains through theradial row assembly 60 of the existing main bearing assembly 10. Upliftrollers in the uplift row assembly 40 of the existing main bearingassembly 10 remain available for potential uplift or overturningmoments.

This embodiment reacts vertical load from the turret structure 12 of theturret into the turret supporting structure 14 of the vessel through theplurality of existing inner ring stud bolts 32 of the bearing inner ring30 as shown in FIGS. 2-4. A spherical washer 118 and a special nut 112,preferably externally and internally threaded, replaces the existingwasher 36 and lower nut 34 on the inner ring stud bolts 32. A coupler110 is threaded onto the special nut 112 at the lower end of theexisting inner ring stud bolt 32. A bearing disk 116 is inserted intothe lower portion of each coupler 110 as shown in FIGS. 2 and 4.Preferably, the bearing disks 116 are made of a self-lubricated,composite material. A set screw 114 locks each coupler 110 to theexisting inner ring stud bolt 32. The height of the coupler 110 withbearing disk 116 is set to form a flat planar lower bearing surface foreven load distribution.

A continuous bearing ring 120 is preferably formed by a plurality ofbearing ring segments. A sliding surface 122, preferably of stainlesssteel, is placed on an upper portion of the bearing ring 120 andpositioned between the coupler bearing disks 116 and the bearing ring120. The sliding surface 122 may be fastened securely to the bearingring 120, as for example, by bolts 124 as shown in FIG. 4. Preferably,the stainless sliding surface 122 is segmented and forms a continuousring that is alternatingly segmented with the segmented bearing ring120. The bearing disks 116 of the couplers 110 are arranged and designedto slide on the stainless sliding surface 122 on the bearing ring 120upon completion of the turret bearing remediation process.

Preferably, a plurality of reaction plates 126 and a plurality ofsupport plates 130 are fastened to the turret head supporting structure14 of the vessel. Typically, the number of reaction plates 126 and thenumber of support plates 130 matches the number of radial stiffeners 16,as for example twenty-four (24). A plurality of holes 18A are drilled ina bottom plate 18 below the turret head supporting structure 14.Preferably, the holes 18A are axially aligned with the holes for theouter ring stud bolts 46. The holes 18A allow the mounting of thesupport plates 130 to an upper surface of the bottom plate 18 and thereaction plates 126 to a lower surface of the bottom plate 18 with newlarge stud bolts 132 extending through aligned holes in the supportplates 130, reaction plates 126 and bottom plate 18. After installingnuts 134, the new large stud bolts 132 are tensioned, preferablyhydraulically with hydraulic tensioner 144 (FIG. 4).

A plurality of spreader bars 136, preferably the same in number as theplurality of support plates 130, may be installed to further support theaxial load of the turret structure 12. Each spreader bar 136 may bepositioned directly above a support plate 130. Preferably, the spreaderbar 136 is connected with a nut 138 to an upper end of the two outermostnew large stud bolts 132 connecting the support plate 130 to the bottomplate 18 as shown in FIGS. 2 and 3. The spreader bar 136 is attached tothe turret head support structure 14 by replacing the existing outerring studs 46, located above and between the axially aligned twooutermost new large stud bolts 132, with new longer outer ring studs 46′(FIG. 2) threaded into the spreader bar 136. Referring to FIG. 3,spacers 140 allow the new longer outer ring studs 46′ to be tensionedwithout over loading the structure. This arrangement forms a stiff loadreacting assembly attached to the existing structure.

A plurality of jack screws 142 are installed in the reaction plates 126below and in contact with the continuous bearing ring 120 as shown inFIGS. 3 and 4. The plain bearing assembly 100 is loaded by turning aplurality of jack screws 142 with a hydraulic torque wrench to aspecified height to lift the turret structure 12 and form a flat surfacefor bearing support.

A preferred method of installing the plain bearing assembly 100 in situwill now be described. The plurality of holes 18A are drilled throughthe bottom plate 18 of the turret supporting structure 14 around itscircumference. The holes 18A are preferably substantially aligned withthe outer ring stud bolts 46. The inner ring stud bolts 32 arede-tensioned one at a time and the washers 36 and lower nuts 34 replacedwith the spherical washers 118 and new special nuts 112. The specialnuts 112 are preferably internally and externally threaded. The innerring stud bolts 32 are re-tensioned such that a predetermined lengthprotrudes below the lower special nuts 112. For example, 10 millimetersof the inner ring stud bolt 32 may protrude below the special nut 112.Referring to FIG. 4, an upper portion 110A of each coupler 110 isinternally threaded, allowing the couplers 110 to be threadablyinstalled onto the lower special nuts 112. The couplers 110 are allpositioned to the same elevation, preferably by laser measurement. A setscrew 114 threadably engaging a threaded lower portion 110B of thecoupler 110 is tightened against the bottom of the inner ring stud bolt32 to maintain the proper elevation of the couplers 110. Theself-lubricated, composite material bearing disks 116 are installed inthe lower end of the couplers 110.

In the preferred embodiment, the reaction plates 126, support plates 130and spreader bars 136 are in sections sized to be aligned and cooperatewith five adjacent outer ring stud bolts 46. For each section, theexisting inner three outer ring stud bolts 46 are removed. The pluralityof support plates 130 are positioned onto the upper surface of thebottom plate 18 with five new large stud bolts 132 received in holes130A extending through each support plate 130. Nuts 134 are attached tothe upper end of the stud bolts 132.

The segments of the continuous bearing ring 120 and the continuousstainless sliding surface 122 are assembled together forming acontinuous ring around the circumference of the turret. Preferably, thecontinuous bearing ring 120 with sliding surface 122 are supported,temporarily on a stand, below the couplers 110.

Individual reaction plates 126, preferably with the jack screws 142installed, are positioned below the bottom plate 18 in alignment with acorresponding support plate 130. The five new large stud bolts 132 inthe corresponding support plate 130 are lowered through the bottom plateholes 18A and through corresponding holes 126A in the reaction plate126. Lower nuts 134 are installed on the lower end of the large studbolts 132 and the stud bolts 132 are tensioned. Preferably, apredetermined length of the large stud bolts 132 protrudes below thelower nuts 134. Once enough reaction plates 126 are installed to supportthe continuous bearing ring 120, the support stands can be removed. Theremaining reaction plates 126 may then be installed.

The spreader bars 136 are installed by lowering the spreader bar 136over the upper ends of the five large stud bolts 132 such that the outerlarge stud bolt 132 at each end extends through an outer lower hole 136Aat each end of the spreader bar 136. A nut 138 is threaded onto theprotruding upper end of the outer large stud bolt 132 and tensioned tosecure the spreader bar 136 to the lower reaction plate 126. The threenew longer outer ring studs 46′ are inserted through the outer upperring 42, outer lower ring 22, turret supporting structure 14, and aspacer 140 before being threaded into a threaded opening of the spreaderbar 136. Referring to FIG. 3, spacers 140 allow the new longer outerring studs 46′ to be tensioned without over loading the structure. Thisarrangement forms a stiff load reacting assembly attached to theexisting structure. The jacking screws 142 are then used to align thecontinuous stainless steel sliding surface 122 with the bearing disks116. The plain bearing assembly 100 is loaded by turning the pluralityof jack screws 142 with a hydraulic torque wrench to a specified heightto lift the turret structure 12 and form a flat surface for bearingsupport. The turret structure 12 is raised to remove the vertical loadfrom the damaged original support row assembly 20.

The above-described embodiment of the plain bearing assembly 100installed below the existing bearing assembly 10 provides the followingbenefits and characteristics:

uses existing inner ring bolting 32 to react load below existing bearingassembly 10;

minimizes hot work (e.g., welding or flame cutting);

uses short lead time materials;

utilizes self-lubricating composite bearing material used on manyapplications;

deflections and tolerances are less of an issue with compliant bearingmaterial;

higher levels of breakout torque required to rotate the chaintable(i.e., turret structure 12);

uses jacking screws 142 to lift the chaintable 12 to original position;and

radial load path remains through the radial row assembly 60 of theexisting bearing assembly 10.

A second preferred embodiment comprises installing a support rollerbearing assembly 200 in situ underneath the existing main bearing 10 asshown in FIGS. 5-7. The support roller bearing assembly 200 solutionshares many of the same components as the plain bearing assembly 100solution so that the planning of both embodiments is available tomaximize uptime of the floating vessel, typically a floating productionstorage and offloading unit (FPSO). The support roller bearing assembly200 solution also removes the vertical and moment load off the existingmain bearing 10 while the radial load path remains through the radialrow assembly 60 of the existing main bearing 10. The uplift row assembly40 in the existing main bearing 10 remains available for potentialuplift or overturning moments. With the use of rollers, the secondpreferred embodiment remains a low torque solution similar to theoriginal design.

As with the plain bearing assembly 100, this embodiment reacts verticalload from the turret structure 12 into the existing inner ring stud bolt32 assembly and into the turret supporting structure 14 of the vessel. Aspherical washer 118 and a special nut 112, preferably externally andinternally threaded, replaces the existing washer 36 and lower nut 34 onthe inner ring stud bolts 32. A coupler 210 is threaded onto the specialnut 112 at the lower end of the existing inner ring stud bolt 32. A setscrew 214 locks each coupler 210 to the existing inner ring stud bolt32. The height of the coupler 210 is set to form a flat planar bearingsurface for even load distribution.

An upper bearing ring 250 is preferably formed by a plurality of upperbearing ring segments. A self-lubricated composite bearing material ring252 is placed into an upper portion of the upper bearing ring 250 toabsorb minute deviations in the height of the couplers 210. The upperbearing ring 250 is segmented to form a continuous ring. Preferably, thebearing material ring 252 is segmented and forms a continuous ring thatis alternatingly segmented with the segmented upper bearing ring 250.

A continuous lower bearing ring 260 is preferably formed by a pluralityof lower bearing ring segments. Hardened and ground steel races 262 areplaced in recesses of the upper bearing ring 250 and the lower bearingring 260 to provide the rolling element surface for new rollers 264separated by cages 266. The lower bearing ring 260 is supported by aplurality of jack screws 242 mounted in the reaction plates 126.

On the turret supporting structure 14 of the vessel side, all of theassembly is identical to the plain bearing assembly 100 embodimentdescribed above with respect to FIGS. 2-4, with the exception of thejack screws 242 which differ slightly. As shown in FIG. 8, preferably aport 244 in the jack screws 242 is in fluid communication with ports 268in the lower bearing ring 260 to provide lubrication to the steel races262, rollers 264 and cages 266 of the support roller bearing assembly200. The stiffening assembly comprising the reaction plates 126, supportplates 130 and spreader bars 136 fastened to the existing turretsupporting structure 14 provides ample support for the rolling elementsand minimizes deflections under load.

This new support roller bearing assembly 200 is also loaded by turningthe plurality of jack screws 242 with a hydraulic torque wrench to aspecified height to lift the turret structure 12 and form a flat surfacefor bearing support.

The preferred method of installing the support roller bearing assembly200 in situ is performed in a similar manner as the plain bearingassembly 100. The plurality of holes 18A are drilled through the bottomplate 18 of the turret supporting structure 14 around its circumferencein the same manner as above. The inner ring stud bolts 32 arede-tensioned one at a time and the washers 36 and lower nuts 34 replacedwith the spherical washers 118 and special nuts 112. The inner ring studbolts 32 are re-tensioned such that a predetermined length protrudesbelow the lower special nuts 112. For example, 10 millimeters of theinner ring stud bolt 32 may protrude below the special nut 112. An upperportion 210A of each coupler 210 is internally threaded, allowing thecouplers 210 to be threadably installed onto the lower special nuts 112.The couplers 210 are all positioned to the same elevation, preferably bylaser measurement. A set screw 214 threadably engaging a threaded lowerportion 210B of the coupler 210 is tightened against the bottom of theinner ring stud bolt 32 to maintain the proper elevation of the couplers210. The height of the coupler 210 is set to form a flat planar bearingsurface for even load distribution.

In the preferred embodiment, the reaction plates 126, support plates 130and spreader bars 136 are in sections sized to be aligned and cooperatewith five adjacent outer ring stud bolts 46. For each section, theexisting inner three outer ring stud bolts 46 are removed. The pluralityof support plates 130 are each positioned onto the upper surface of thebottom plate 18 with five new large stud bolts 132 received in holes130A extending through each support plate 130. Nuts 134 are attached tothe upper end of the stud bolts 132.

The segments of the continuous lower bearing ring 260 are joinedtogether and the hardened and ground steel race segments 262 areinstalled in the upper recess of the continuous lower bearing ring 260.The steel race segments 262 are alternatingly segmented with the lowerbearing ring segments 260. The continuous lower bearing ring 260 withcontinuous steel race 262 are assembled forming a continuous ring aroundthe circumference of the turret.

The segments of the continuous upper bearing ring 250 are joinedtogether and the self-lubricated composite bearing material ringsegments 252 are placed into the upper portion of the upper bearing ring250. The bearing material ring segments 252 are alternatingly segmentedwith the upper bearing ring segments 250. The hardened and ground steelrace segments 262 are installed in the lower recess of the continuousupper bearing ring 250. The steel race segments 262 are alternatinglysegmented with the upper bearing ring segments 250. In a preferredembodiment, the upper bearing ring 250 comprises top upper bearingsegments 250A and bottom upper bearing ring segments 250B which arealternatingly segmented and fastened together to form the continuousupper bearing ring 250.

Referring to FIG. 8, the new support rollers 264 and cages 266 areinstalled between the upper and lower support races 262 in the lower andupper recesses of the upper bearing ring 250 and the lower bearing ring260. Preferably, the assembled upper and lower bearing rings 250 and 260with the support rollers 264, cage 266 and races 262 are supported,temporarily on a stand, below the couplers 210.

Individual reaction plates 126, preferably with the jack screws 242installed, are positioned below the bottom plate 18 in alignment with acorresponding support plate 130. The five new large stud bolts 132 inthe corresponding support plate 130 are lowered through the bottom plateholes 18A and through corresponding holes 126A in the reaction plate126. Lower nuts 134 are installed on the lower end of the large studbolts 132 and the stud bolts 132 are tensioned. Preferably, apredetermined length of the large stud bolts 132 protrudes below thelower nuts 134. Once enough reaction plates 126 are installed to supportthe assembled upper and lower bearing rings 250 and 260 with the supportrollers 264, cage 266 and races 262, the support stands can be removed.The remaining reaction plates 126 may then be installed.

The spreader bars 136 are installed by lowering the spreader bar 136over the upper ends of the five large stud bolts 132 such that the outerlarge stud bolt 132 at each end extends through an outer lower hole 136Aat each end of the spreader bar 136. A nut 138 is threaded onto theprotruding upper end of the outer large stud bolt 132 and tensioned tosecure the spreader bar 136 to the lower reaction plate 126. The threenew longer outer ring studs 46′ are inserted through the outer upperring 42, outer lower ring 22, turret supporting structure 14, and aspacer 140 before being threaded into a threaded opening of the spreaderbar 136. The spacers 140 allow the new longer outer ring studs 46′ to betensioned without over loading the structure. This arrangement forms astiff load reacting assembly attached to the existing structure. Thejacking screws 242 are then used to align the upper bearing materialring 252 of the upper bearing ring 250 with the couplers 210. Thesupport roller bearing assembly 200 is loaded by turning the pluralityof jack screws 242 with a hydraulic torque wrench to a specified heightto lift the turret structure 12 and form a flat surface for bearingsupport. The turret structure 12 is raised to remove the vertical loadfrom the damaged original support row assembly 20.

The embodiment of the support roller bearing assembly 200 installedbelow the existing bearing assembly 10 provides the following benefitsand characteristics:

uses existing inner race bolting 32 to react load below existing bearingassembly 10;

minimizes hot work;

uses short lead time materials with the exception of possibly therollers 264 and hardened races 262;

utilizes rollers 264 riding on hardened races 262 similar to those usedin segmented bearings;

deflections and tolerances which are more of an issue for roller loadingis aided by the bearing material ring 252;

low level of breakout torque required to rotate the chaintable (i.e.,turret structure 12);

uses jacking screws 242 to lift the chaintable 12 to original position;and

radial load path remains through the radial row assembly 60 of theexisting bearing assembly 10.

While the invention has been described in detail above with reference tospecific embodiments, it will be understood that modifications andalterations in the embodiments disclosed may be made by those practicedin the art without departing from the spirit and scope of the invention.All such modifications and alterations are intended to be covered. Inaddition, all publications cited herein are indicative of the level ofskill in the art and are hereby incorporated by reference in theirentirety as if each had been individually incorporated by reference andfully set forth.

What is claimed is:
 1. A deployable assembly for in-situ remediation ofa support row assembly supporting an axial load of a turret on a turretsupporting structure of a floating vessel, comprising: a support bearingassembly comprising an upper bearing surface, a lower bearing surface,and a plurality of bearings, wherein: the plurality of bearings areconfigured to be disposed between the upper bearing surface and thelower bearing surface, the lower bearing surface is an upper surface ofa bearing ring, the bearing ring is configured to be located around acircumference of the turret, and the plurality of bearings areconfigured to support the axial load upon installation of the supportbearing assembly.
 2. The deployable assembly of claim 1, wherein: thelower bearing surface is an upper surface of a first bearing ring, theupper bearing surface is a lower surface of a second bearing ring, andthe plurality of bearings are configured to move on the lower bearingsurface or the upper bearing surface.
 3. The deployable assembly ofclaim 1, wherein: the upper bearing surface is a lower surface of aplurality of couplers configured to be secured to the turret by aplurality of inner ring fasteners coupled to the turret, and theplurality of bearings are configured to move on the lower bearingsurface or the upper bearing surface.
 4. The deployable assembly ofclaim 1, wherein the plurality of bearings are configured to move on thelower bearing surface.
 5. The deployable assembly of claim 1, whereinthe plurality of bearings are a plurality of bearing pads configured toslide on the lower bearing surface or the upper bearing surface.
 6. Thedeployable assembly of claim 5, wherein the plurality of bearings aredisposed on the upper bearing surface and configured to slide on thelower bearing surface.
 7. The deployable assembly of claim 1, whereinthe plurality of bearings are a plurality of roller bearings configuredto roll on the lower bearing surface and the upper bearing surface. 8.The deployable assembly of claim 1, further comprising a plurality ofreaction plates configured to support the axial load upon installationof the support bearing assembly.
 9. The deployable assembly of claim 1,wherein the support row assembly comprises a roller bearing assemblydisposed between an inner ring connected to the turret and an outer ringconnected to the vessel.
 10. The deployable assembly of claim 9, whereinthe inner ring is secured to the turret by a plurality of inner ringfasteners, and wherein the outer ring is secured to the vessel by aplurality of outer ring fasteners.
 11. The deployable assembly of claim10, wherein the support bearing assembly is configured to couple to oneor more of the plurality of inner ring fasteners.
 12. The deployableassembly of claim 10, wherein the support bearing assembly is configuredto support the axial load through one or more of the plurality of innerring fasteners.
 13. The deployable assembly of claim 1, furthercomprising a plurality of reaction plates, wherein the plurality ofreaction plates, the lower bearing surface, the plurality of bearings,and the upper bearing surface are configured to support the axial loadupon installation of the support bearing assembly.
 14. The deployableassembly of claim 1, further comprising a plurality of jack screws or aplurality of hydraulic jacks configured to move the turret such that theaxial load is removed from the support row assembly and transferred tothe support bearing assembly.
 15. A deployable assembly for in-situremediation of a support row assembly supporting an axial load of aturret on a turret supporting structure of a floating vessel,comprising: a support bearing assembly comprising a plurality ofcouplers, a plurality of reaction plates, and a plurality of bearings,wherein: the plurality of bearings are a plurality of bearing pads or aplurality of roller bearings, the plurality of reaction plates and theplurality of couplers are configured to support the plurality ofbearings therebetween, and the plurality of reaction plates, theplurality of couplers, and the plurality of bearings are configured tosupport the axial load of the turret upon installation of the supportbearing assembly.
 16. The deployable assembly of claim 15, wherein theplurality of couplers are configured to be secured to a plurality ofinner ring fasteners coupled to the turret.
 17. The deployable assemblyof claim 16, further comprising a bearing ring, wherein: the bearingring is configured to be disposed between the plurality of reactionplates and the plurality of couplers, and the plurality of bearings areconfigured to move on an upper surface of the bearing ring.
 18. Thedeployable assembly of claim 15, further comprising a bearing ringconfigured to be located around a circumference of the turret betweenthe plurality of reaction plates and the plurality of couplers, whereinthe plurality of bearings are configured to move on a surface of thebearing ring.
 19. The deployable assembly of claim 15, furthercomprising a plurality of jack screws or a plurality of hydraulic jacksconfigured to move the turret such that the axial load is removed fromthe support row assembly and transferred to the support bearingassembly.
 20. A process for remediating a support row assemblysupporting an axial load of a turret on a turret supporting structure ofa floating vessel, comprising: installing a support bearing assemblyaround a circumference of the turret, the support bearing assemblycomprising an upper bearing surface, a lower bearing surface, and aplurality of bearings disposed between the upper bearing surface and thelower bearing surface; and transferring the axial load of the turretfrom the support row assembly to the plurality of bearings uponinstallation of the support bearing assembly.